US4246218A - Process for the manufacture of a piece comprising at least one porous abradable material - Google Patents
Process for the manufacture of a piece comprising at least one porous abradable material Download PDFInfo
- Publication number
- US4246218A US4246218A US06/059,751 US5975179A US4246218A US 4246218 A US4246218 A US 4246218A US 5975179 A US5975179 A US 5975179A US 4246218 A US4246218 A US 4246218A
- Authority
- US
- United States
- Prior art keywords
- mold
- mixture
- support part
- powders
- porous material
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/11—Making porous workpieces or articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
- B22F1/09—Mixtures of metallic powders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/002—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of porous nature
- B22F7/004—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of porous nature comprising at least one non-porous part
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
- F01D11/125—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material with a reinforcing structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12028—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
- Y10T428/12042—Porous component
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12028—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
- Y10T428/12063—Nonparticulate metal component
- Y10T428/12069—Plural nonparticulate metal components
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12028—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
- Y10T428/12063—Nonparticulate metal component
- Y10T428/12069—Plural nonparticulate metal components
- Y10T428/12076—Next to each other
Definitions
- the present invention concerns formed pieces comprising at least one portion of a porous abradable material and the process for the preparation of said pieces.
- abradables are materials subject to wear by abrasion, they are used in particular as linings in turbine housings to limit the clearance at the tip of the blades.
- abradable materials employed at elevated temperatures are frequently porous materials wherein a metallic piece may cut an impression due to the shifting of said piece and to the friction of the piece against these materials.
- porous materials are available in the form of plates, which most frequently are shaped and mounted on a support. This shaping and mounting process poses difficult industrial problems.
- the present invention concerns a process for the preparation of shaped pieces at least portions of which are of an abradable material.
- Said pieces may consists solely of the abradable material or they may comprise, as a support and/or as an internal partition, a part joined by brazing to said material and consisting of a metal or an alloy.
- the process according to the invention is characterized by a mold being used wherein the synthesis of the abradable material is effected by diffusion. Synthesis by diffusion may be effected advantageously by the process described in the application Ser. No. 58,487 filed July 18, 1979 by the present applicant for a "novel porous body and process for its preparation".
- said mold is filled with a mixture of powders, one of which represents 85 to 99.5% by weight of the mixture and is a base material selected from the group consisting of nickel, cobalt, iron and various alloys of these metals, and a fusible and diffusible material chosen from tin, indium, gallium, germanium, antimony, together with the mixtures and alloys of said metals and the mold is subsequently heated in a controlled atmosphere, at a temperature and for the period of time sufficient to cause a bond to be formed between the powder particles of the base metals by means of diffusion brazing.
- a mixture of powders one of which represents 85 to 99.5% by weight of the mixture and is a base material selected from the group consisting of nickel, cobalt, iron and various alloys of these metals, and a fusible and diffusible material chosen from tin, indium, gallium, germanium, antimony, together with the mixtures and alloys of said metals and the mold is subsequently heated in a controlled atmosphere, at a temperature and
- the abradable material is prepared in a mold having a shape corresponding to the shape of the final piece desired; because the abradable material is synthesized in a mold by means of the diffusion of the particles of the base material, it is conceivable that depending on the material constituting the mold, said mold itself may be bonded by its entire internal surface of by a part of said internal surface, to the abradable material being synthesized and that it thus may constitute, in its entirety or in part, a portion of the final piece to carry the abradable material; it is equally conceivable that inside the mold and prior to the introduction of the powders, various metal partitions may be conveniently introduced and positioned, said partitions being locked in and bonded to the abradable material synthetized in the mold.
- the materials used to prepare the abradable materials are in the form of powders with grain sizes of between 80 and 220 microns. Diffusion takes place in a controlled atmosphere, i.e., in an inert gas atmosphere or in a vacuum.
- the powder mixture is not subjected to an external pressure, other than a possible pressure of the inert gas, during heating.
- diffusion brazing is obtained by heating to a temperature higher than the melting temperature of the fusible material but lower than the solidus of the base material. The duration of heating is considered sufficient when, for a given temperature, the entirety of the fusible material has diffused within the base material.
- the shaped piece consists solely of the abradable material.
- a mold for example, one that may be dismantled, having walls prepared so that the powders do not adhere to said walls during the process of the preparation of the abradable material.
- the mold may have, for example, walls lined with alumina or with a known antiwetting agent.
- the finished piece comprises a part of an abradable material synthesized in situ and a part consisting of a mold or a part of the mold and/or at least one metal partition located at least in part within the abradable material.
- the fusible material present in the powder mixture will perform not only the function of diffusion brazing the base material in the form of a powder, but also functions to diffusion braze said base material to the mold and/or the partition.
- the conditions under which the process according to the invention is effected will have to take into account this new role of the fusible material in relation to the mold and/or the partition.
- the non-limiting examples following hereinbelow will serve to illustrate the invention.
- a mixutre is prepared of 95% by weight of a powder of an 80/20 nickel-chromium alloy (grain size: 80 to 140 microns) with 5% by weight of a powder of tin with an average grain size or approximately 150 microns; after homogenization, the mixture is poured in the cavity of a mold consisting of a bottom support of KC20WN, the upper surface whereof is lined with alumina upon which four blocks of KC20WN are conveniently placed, said blocks also having the facing surfaces lined with alumina.
- the material referred to above as KC20WN is a cobalt based alloy containing about 20% of chromium, 15% tungsten, 10% nickel and about 0.4% of silicon.
- the material is also sold in the United States by the CABOT Company, under the designation HS25.
- the assembly is placed in a furnace wherein a vacuum of 10 -3 Pa is maintained and then heated at 1125° C. for 15 minutes. After cooling, the mold is dismantled and a specimen of an abradable material with a density of approximately 3.2 obtained.
- FIG. 1 is a sectional view of a mold and a partition
- FIG. 2 is a sectional view of the mold of FIG. 1 at a later stage of the process.
- a mold having the form shown in a transverse section in FIG. 1, is prepared.
- the metallic support to which the porous abradable material is to be mounted consists of a ferrule 1.
- the mold is further bounded by a bottom 2 and an internal ferrule 3.
- a homogeneous mixture of 95% by weight of a powder of an 80/20 nickel-chromium alloy with an average grain size of 80-140 microns, with 5% by weight of a powder of tin with an average grain size of approximately 150 microns, is prepared.
- a portion of said mixture is introduced in the cavity 4 of the mold (the cavity having the form of a torus with a rectangular section).
- a partition 5 is introduced therein, said partition being of a circular form with an external diameter substantially equal to the internal diameter of the ferrule 1.
- the periphery of the partition 5 is equipped with a gold-nickel wire assuring its subsequent brazing to the ferrule 1 with satisfactory tightness.
- the remaining portion of the powder mixture is poured in so as to completely fill the cavity of the mold.
- the assembly is placed in a furnace under vacuum (pressure less than 10 -3 Pa then heated to 1125° C. for 15 minutes approximately.
- parts 2 and 3 are removed by means of turning while leaving--as shown in FIG. 2, the support 1 clad by the abradable material 6, including the partition 5.
- the parts 2 and 3 may be present in the form of removable tooling lined with an antiwetting agent, such as alumina.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- Powder Metallurgy (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
- Polishing Bodies And Polishing Tools (AREA)
Abstract
The invention concerns a process for the manufacture of pieces comprising least one part of an abradable, porous material, which may be integral with a support part. The process is characterized in that synthesis by diffusion of the abradable material is effected in a mold, at least one part of which constitutes the support piece.
Description
The present invention concerns formed pieces comprising at least one portion of a porous abradable material and the process for the preparation of said pieces.
It is known that abradables are materials subject to wear by abrasion, they are used in particular as linings in turbine housings to limit the clearance at the tip of the blades. Such abradable materials employed at elevated temperatures, are frequently porous materials wherein a metallic piece may cut an impression due to the shifting of said piece and to the friction of the piece against these materials. Such porous materials are available in the form of plates, which most frequently are shaped and mounted on a support. This shaping and mounting process poses difficult industrial problems. Furthermore, it is often desirable, for cooling purposes, to place internal partitions in these materials, which are difficult to apply with conventional materials.
The present invention concerns a process for the preparation of shaped pieces at least portions of which are of an abradable material. Said pieces may consists solely of the abradable material or they may comprise, as a support and/or as an internal partition, a part joined by brazing to said material and consisting of a metal or an alloy.
The process according to the invention is characterized by a mold being used wherein the synthesis of the abradable material is effected by diffusion. Synthesis by diffusion may be effected advantageously by the process described in the application Ser. No. 58,487 filed July 18, 1979 by the present applicant for a "novel porous body and process for its preparation". According to this process, said mold is filled with a mixture of powders, one of which represents 85 to 99.5% by weight of the mixture and is a base material selected from the group consisting of nickel, cobalt, iron and various alloys of these metals, and a fusible and diffusible material chosen from tin, indium, gallium, germanium, antimony, together with the mixtures and alloys of said metals and the mold is subsequently heated in a controlled atmosphere, at a temperature and for the period of time sufficient to cause a bond to be formed between the powder particles of the base metals by means of diffusion brazing.
Thus, according to the invention, the abradable material is prepared in a mold having a shape corresponding to the shape of the final piece desired; because the abradable material is synthesized in a mold by means of the diffusion of the particles of the base material, it is conceivable that depending on the material constituting the mold, said mold itself may be bonded by its entire internal surface of by a part of said internal surface, to the abradable material being synthesized and that it thus may constitute, in its entirety or in part, a portion of the final piece to carry the abradable material; it is equally conceivable that inside the mold and prior to the introduction of the powders, various metal partitions may be conveniently introduced and positioned, said partitions being locked in and bonded to the abradable material synthetized in the mold.
The materials used to prepare the abradable materials are in the form of powders with grain sizes of between 80 and 220 microns. Diffusion takes place in a controlled atmosphere, i.e., in an inert gas atmosphere or in a vacuum. The powder mixture is not subjected to an external pressure, other than a possible pressure of the inert gas, during heating.
In the case when an auxiliary powder of a fusible material is used, diffusion brazing is obtained by heating to a temperature higher than the melting temperature of the fusible material but lower than the solidus of the base material. The duration of heating is considered sufficient when, for a given temperature, the entirety of the fusible material has diffused within the base material.
In one mode of embodiment of the invention, the shaped piece consists solely of the abradable material. In such a case a mold, for example, one that may be dismantled, having walls prepared so that the powders do not adhere to said walls during the process of the preparation of the abradable material. The mold may have, for example, walls lined with alumina or with a known antiwetting agent.
In another mode of embodiment of the invention, the finished piece comprises a part of an abradable material synthesized in situ and a part consisting of a mold or a part of the mold and/or at least one metal partition located at least in part within the abradable material. In this case, the fusible material present in the powder mixture will perform not only the function of diffusion brazing the base material in the form of a powder, but also functions to diffusion braze said base material to the mold and/or the partition. The conditions under which the process according to the invention is effected will have to take into account this new role of the fusible material in relation to the mold and/or the partition. The non-limiting examples following hereinbelow will serve to illustrate the invention.
A mixutre is prepared of 95% by weight of a powder of an 80/20 nickel-chromium alloy (grain size: 80 to 140 microns) with 5% by weight of a powder of tin with an average grain size or approximately 150 microns; after homogenization, the mixture is poured in the cavity of a mold consisting of a bottom support of KC20WN, the upper surface whereof is lined with alumina upon which four blocks of KC20WN are conveniently placed, said blocks also having the facing surfaces lined with alumina. The material referred to above as KC20WN is a cobalt based alloy containing about 20% of chromium, 15% tungsten, 10% nickel and about 0.4% of silicon. The material is also sold in the United States by the CABOT Company, under the designation HS25. The assembly is placed in a furnace wherein a vacuum of 10-3 Pa is maintained and then heated at 1125° C. for 15 minutes. After cooling, the mold is dismantled and a specimen of an abradable material with a density of approximately 3.2 obtained.
This example will be described with reference to the schematic drawings attached hereto wherein:
FIG. 1 is a sectional view of a mold and a partition;
FIG. 2 is a sectional view of the mold of FIG. 1 at a later stage of the process.
A mold having the form shown in a transverse section in FIG. 1, is prepared. The metallic support to which the porous abradable material is to be mounted, consists of a ferrule 1. The mold is further bounded by a bottom 2 and an internal ferrule 3.
A homogeneous mixture of 95% by weight of a powder of an 80/20 nickel-chromium alloy with an average grain size of 80-140 microns, with 5% by weight of a powder of tin with an average grain size of approximately 150 microns, is prepared. A portion of said mixture is introduced in the cavity 4 of the mold (the cavity having the form of a torus with a rectangular section). When the cavity 4 is filled to about one-half of its height, a partition 5 is introduced therein, said partition being of a circular form with an external diameter substantially equal to the internal diameter of the ferrule 1. The periphery of the partition 5 is equipped with a gold-nickel wire assuring its subsequent brazing to the ferrule 1 with satisfactory tightness. Thereafter, the remaining portion of the powder mixture is poured in so as to completely fill the cavity of the mold. The assembly is placed in a furnace under vacuum (pressure less than 10-3 Pa then heated to 1125° C. for 15 minutes approximately. After cooling, parts 2 and 3 are removed by means of turning while leaving--as shown in FIG. 2, the support 1 clad by the abradable material 6, including the partition 5. In a variant of embodiment, the parts 2 and 3 may be present in the form of removable tooling lined with an antiwetting agent, such as alumina.
Claims (3)
1. Process for the manufacture of shaped pieces comprising a first part of a porous material subject to wear by abrasion and a second support part of a solid material, comprising the steps of: providing a mold, at least one part of which constitutes a support part, coating the internal surface of the other parts with an antiwetting agent, effecting synthesis of the porous material and its bonding to the support part by filling said mold with a homogeneous mixture of two powders, one of which, representing 80 to 99.5% by weight of the mixture, is a base material selected from the group consisting of nickel, cobalt, iron and different alloys of these metals, and the other, representing 0.5% to 20% by weight of the mixture, is a fusible material capable of diffusion and chosen from the group consisting of tin, indium, gallium, germanium, antimony, together with mixtures and alloys of said metals and by heating said mold in a controlled atmosphere, at a temperature higher then 900° C. but in all cases lower than the solidus of the base material and the material of the mold, for a sufficient period of time to permit the migration of the fusible material and the bonding, by means of diffusion brazing, of the grains of the powder to each other and to the support part.
2. Process according to claim 1, wherein the final shape of the piece is obtained by removing the parts of the mold walls not bonded to the said porous material.
3. Process according to one of claims 1 or 2 wherein, during the filling of the mold with the mixture of the two powders, at least one partition is inserted into said powders, which is bonded to the porous material during the synthesis of the latter.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7821895 | 1978-07-25 | ||
| FR7821895A FR2431896A1 (en) | 1978-07-25 | 1978-07-25 | PROCESS FOR THE MANUFACTURE OF PARTS COMPRISING AT LEAST ONE PART OF A POROUS MATERIAL LIKELY TO BE ABRASIONALLY USED |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US4246218A true US4246218A (en) | 1981-01-20 |
Family
ID=9211108
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US06/059,751 Expired - Lifetime US4246218A (en) | 1978-07-25 | 1979-07-23 | Process for the manufacture of a piece comprising at least one porous abradable material |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4246218A (en) |
| DE (1) | DE2930217A1 (en) |
| FR (1) | FR2431896A1 (en) |
| GB (1) | GB2027747B (en) |
| SE (1) | SE446604B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105081622A (en) * | 2015-09-14 | 2015-11-25 | 沈阳飞机工业(集团)有限公司 | Method for manufacturing and pre-installing brazing filler material ring |
| CN105290405A (en) * | 2015-11-09 | 2016-02-03 | 东睦新材料集团股份有限公司 | Manufacturing method of powder metallurgy part with sealing cavity |
| CN105312570A (en) * | 2014-06-05 | 2016-02-10 | 华中科技大学 | Increment manufacturing method for part or mold |
| CN109093123A (en) * | 2018-09-12 | 2018-12-28 | 北京恒源天桥粉末冶金有限公司 | A kind of preparation method of Combined filter element |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19747242C2 (en) * | 1997-10-25 | 2002-02-21 | Abb Patent Gmbh | Process for producing a metal mold for vacuum chamber screens or vacuum chamber contact pieces |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB611818A (en) | 1946-05-09 | 1948-11-04 | Vandervell Products Ltd | Improvements in bearings |
| FR949279A (en) | 1940-03-07 | 1949-08-25 | Gen Motors Corp | Improved process for manufacturing porous metal objects and resulting products |
| US3369879A (en) * | 1964-11-19 | 1968-02-20 | Super Cut | Method of making a peripheral diamond grinding wheel |
| US3664819A (en) * | 1969-11-14 | 1972-05-23 | Norton Co | Resin bonded metal-coated diamond or cubic boron nitride abrasive tools containing an inorganic crystalline filler and graphite |
| US3756796A (en) * | 1967-12-13 | 1973-09-04 | Super Cut | Method of forming a peripheral grinding wheel |
| US3829299A (en) * | 1972-04-10 | 1974-08-13 | Engis Corp | Molded abrasive article of iron-silicon alloy,and diamond powder |
| GB1412415A (en) | 1971-12-03 | 1975-11-05 | Atomic Energy Authority Uk | Metal powder compacts |
| US4024675A (en) * | 1974-05-14 | 1977-05-24 | Jury Vladimirovich Naidich | Method of producing aggregated abrasive grains |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA963497A (en) * | 1970-12-21 | 1975-02-25 | Gould Inc. | Powder metal honeycomb |
-
1978
- 1978-07-25 FR FR7821895A patent/FR2431896A1/en active Granted
-
1979
- 1979-07-23 US US06/059,751 patent/US4246218A/en not_active Expired - Lifetime
- 1979-07-24 SE SE7906334A patent/SE446604B/en not_active IP Right Cessation
- 1979-07-24 GB GB7925771A patent/GB2027747B/en not_active Expired
- 1979-07-25 DE DE19792930217 patent/DE2930217A1/en active Granted
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR949279A (en) | 1940-03-07 | 1949-08-25 | Gen Motors Corp | Improved process for manufacturing porous metal objects and resulting products |
| GB611818A (en) | 1946-05-09 | 1948-11-04 | Vandervell Products Ltd | Improvements in bearings |
| US3369879A (en) * | 1964-11-19 | 1968-02-20 | Super Cut | Method of making a peripheral diamond grinding wheel |
| US3756796A (en) * | 1967-12-13 | 1973-09-04 | Super Cut | Method of forming a peripheral grinding wheel |
| US3664819A (en) * | 1969-11-14 | 1972-05-23 | Norton Co | Resin bonded metal-coated diamond or cubic boron nitride abrasive tools containing an inorganic crystalline filler and graphite |
| GB1412415A (en) | 1971-12-03 | 1975-11-05 | Atomic Energy Authority Uk | Metal powder compacts |
| US3829299A (en) * | 1972-04-10 | 1974-08-13 | Engis Corp | Molded abrasive article of iron-silicon alloy,and diamond powder |
| US4024675A (en) * | 1974-05-14 | 1977-05-24 | Jury Vladimirovich Naidich | Method of producing aggregated abrasive grains |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105312570A (en) * | 2014-06-05 | 2016-02-10 | 华中科技大学 | Increment manufacturing method for part or mold |
| CN105081622A (en) * | 2015-09-14 | 2015-11-25 | 沈阳飞机工业(集团)有限公司 | Method for manufacturing and pre-installing brazing filler material ring |
| CN105290405A (en) * | 2015-11-09 | 2016-02-03 | 东睦新材料集团股份有限公司 | Manufacturing method of powder metallurgy part with sealing cavity |
| CN109093123A (en) * | 2018-09-12 | 2018-12-28 | 北京恒源天桥粉末冶金有限公司 | A kind of preparation method of Combined filter element |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2431896B1 (en) | 1982-04-02 |
| DE2930217C2 (en) | 1990-03-22 |
| FR2431896A1 (en) | 1980-02-22 |
| GB2027747B (en) | 1982-10-27 |
| SE446604B (en) | 1986-09-29 |
| GB2027747A (en) | 1980-02-27 |
| SE7906334L (en) | 1980-01-26 |
| DE2930217A1 (en) | 1980-02-07 |
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